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    Physics III

    Summary

    Prof. Dr. Simon Lilly

    Autor

    Thomas Gersdorf

    ETH Zurich, HS 2008

    $Id: physik_iii.tex 800 2008-12-07 20:46:56Z [email protected] $

    Comitted: Monday 8th December, 2008 Revision 32

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    Contents

    Contents 2

    1 Basics 7

    1 Literature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 72 Constants and Units . . . . . . . . . . . . . . . . . . . . . . . . 7

    2.1 Constants . . . . . . . . . . . . . . . . . . . . . . . . . . 72.2 Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

    3 Terms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 84 Concept of charge . . . . . . . . . . . . . . . . . . . . . . . . . . 8

    2 Electrostatics 9

    1 Force . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 91.1 Coulombs Law . . . . . . . . . . . . . . . . . . . . . . . 91.2 Energy of a charge . . . . . . . . . . . . . . . . . . . . . 9

    2 Eletric field . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 102.1 Charge density . . . . . . . . . . . . . . . . . . . . . . . 102.2 Curl of the electric field . . . . . . . . . . . . . . . . . . 11

    3 Flux . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 113.1 Flux and E-Fields of various charge distributions . . . 11

    4 Gauss Law . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 124.1 integral form . . . . . . . . . . . . . . . . . . . . . . . . 124.2 differential form . . . . . . . . . . . . . . . . . . . . . . 12

    5 Potential . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 135.1 Definiton of potential 0 . . . . . . . . . . . . . . . . . . 135.2 Potential of radial-symmetrical charge distribution . . 13

    5.3 Potential of multiple charges . . . . . . . . . . . . . . . 135.4 Potential of a spherical shell . . . . . . . . . . . . . . . 145.5 Potential of an electric dipole . . . . . . . . . . . . . . . 14

    6 Energy of an electric field . . . . . . . . . . . . . . . . . . . . . 14

    3 Conductors 15

    1 Conductors and Insulators . . . . . . . . . . . . . . . . . . . . . 152 General Electrostatic Problem . . . . . . . . . . . . . . . . . . . 153 Uniqueness Theorem . . . . . . . . . . . . . . . . . . . . . . . . 154 Potential and Field inside an empty cavity in a closed conductor 16

    2

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    5 Mirror principle . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

    6 conducting sphere in external field . . . . . . . . . . . . . . . . 167 Capicatance and capacitors . . . . . . . . . . . . . . . . . . . . 17

    7.1 Definition of capicatance . . . . . . . . . . . . . . . . . 177.2 Types of capacitors . . . . . . . . . . . . . . . . . . . . . 177.3 Energy stored in a capicator . . . . . . . . . . . . . . . 187.4 Systems of capicators . . . . . . . . . . . . . . . . . . . 18

    4 Currents 19

    1 Electric currents . . . . . . . . . . . . . . . . . . . . . . . . . . . 191.1 Definition of the current . . . . . . . . . . . . . . . . . . 19

    2 Ohms law and Resistance . . . . . . . . . . . . . . . . . . . . . 20

    2.1 Resistance and conductivity . . . . . . . . . . . . . . . . 202.2 Definiton of the resistance . . . . . . . . . . . . . . . . . 20

    3 Resistance for various components . . . . . . . . . . . . . . . . 213.1 Discrete component . . . . . . . . . . . . . . . . . . . . 213.2 Spherical conductors . . . . . . . . . . . . . . . . . . . . 213.3 Cylindrical conductiors . . . . . . . . . . . . . . . . . . 21

    4 Resistances in circuits . . . . . . . . . . . . . . . . . . . . . . . 214.1 Parallel circuits . . . . . . . . . . . . . . . . . . . . . . . 214.2 Series circuits . . . . . . . . . . . . . . . . . . . . . . . . 224.3 Combined series and parallel circuits . . . . . . . . . . 22

    5 Energy dissipation . . . . . . . . . . . . . . . . . . . . . . . . . 23

    6 Sources of electromotive force: Voltaic cell . . . . . . . . . . . 237 Circuits with capicators . . . . . . . . . . . . . . . . . . . . . . 23

    5 Fields of moving charges 24

    1 General force on a moving charge . . . . . . . . . . . . . . . . 242 Charge invariance . . . . . . . . . . . . . . . . . . . . . . . . . . 243 Fields of moving charges . . . . . . . . . . . . . . . . . . . . . . 244 Electric field for an accelarated charge . . . . . . . . . . . . . . 245 Forces between moving charges - the magnetic force . . . . . 25

    6 Magnetic fields 26

    1 Definition of magnetic field . . . . . . . . . . . . . . . . . . . . 261.1 Lorentz force . . . . . . . . . . . . . . . . . . . . . . . . 261.2 Definition of B-field . . . . . . . . . . . . . . . . . . . . 26

    2 Force between two wires . . . . . . . . . . . . . . . . . . . . . . 273 Properties of the magnetic field . . . . . . . . . . . . . . . . . . 27

    3.1 Amperes Law . . . . . . . . . . . . . . . . . . . . . . . 274 Magntic poles . . . . . . . . . . . . . . . . . . . . . . . . . . . . 285 Uniqueness theorem . . . . . . . . . . . . . . . . . . . . . . . . 286 Vector potential . . . . . . . . . . . . . . . . . . . . . . . . . . . 28

    6.1 Deduction . . . . . . . . . . . . . . . . . . . . . . . . . . 28

    3

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    Contents

    6.2 General formula . . . . . . . . . . . . . . . . . . . . . . 29

    6.3 Application to a current carrying wire . . . . . . . . . 296.4 General differentials . . . . . . . . . . . . . . . . . . . . 30

    7 Fields of rings and solenoids . . . . . . . . . . . . . . . . . . . 308 Change in B across a current sheet . . . . . . . . . . . . . . . . 31

    8.1 Energy density . . . . . . . . . . . . . . . . . . . . . . . 319 Hall effect . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3210 How do E and B transform together? . . . . . . . . . . . . . . 33

    10.1 Derivation . . . . . . . . . . . . . . . . . . . . . . . . . . 3310.2 General transformation . . . . . . . . . . . . . . . . . . 34

    7 Magnetic Induction 35

    1 Magnetic Induction . . . . . . . . . . . . . . . . . . . . . . . . . 351.1 Isolated conductor . . . . . . . . . . . . . . . . . . . . . 351.2 Loop of wire . . . . . . . . . . . . . . . . . . . . . . . . 35

    2 EMF - Electro motive force . . . . . . . . . . . . . . . . . . . . 362.1 General emf (electro-motive force) . . . . . . . . . . . . 36

    3 Magnetic flux . . . . . . . . . . . . . . . . . . . . . . . . . . . . 364 Faradays law of induction . . . . . . . . . . . . . . . . . . . . . 37

    4.1 Derivation . . . . . . . . . . . . . . . . . . . . . . . . . . 375 Lenz Law . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 386 Mutual inductance . . . . . . . . . . . . . . . . . . . . . . . . . 387 Self inductance . . . . . . . . . . . . . . . . . . . . . . . . . . . 39

    7.1 Circuits with self-inductance . . . . . . . . . . . . . . . 398 Energy in a magnetic field . . . . . . . . . . . . . . . . . . . . . 40

    8.1 General term for any B-field . . . . . . . . . . . . . . . 408.2 Derivation of the energy stored in a solenoid . . . . . . 40

    9 Application: Magnetic field brake . . . . . . . . . . . . . . . . 40

    8 Alternating Currents 42

    1 Definitions for AC-circuits . . . . . . . . . . . . . . . . . . . . . 421.1 Quality factor . . . . . . . . . . . . . . . . . . . . . . . . 42

    2 RCL circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 423 over-damped RCL-circuit . . . . . . . . . . . . . . . . . . . . . 43

    4 RL-Circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 435 RC-circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 446 RLC-circuit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 447 Application: Media player . . . . . . . . . . . . . . . . . . . . . 458 AC currents and voltages as complex numbers . . . . . . . . . 459 Power consumptation in AC current . . . . . . . . . . . . . . . 4710 Some other definition . . . . . . . . . . . . . . . . . . . . . . . . 48

    9 Maxwells equations and electromagnetic waves 49

    1 Previous equations we have met . . . . . . . . . . . . . . . . . 49

    4

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    2 Maxwells Equation . . . . . . . . . . . . . . . . . . . . . . . . . 50

    3 Electromagnetic Waves . . . . . . . . . . . . . . . . . . . . . . . 504 Energy transport in electromagnetic waves . . . . . . . . . . . 515 Lorentz transformations of electromagnetic waves . . . . . . . 52

    10 Electric and Magnetic Fields in Mattter 531 Dielectric Materials . . . . . . . . . . . . . . . . . . . . . . . . . 532 electric dipoles . . . . . . . . . . . . . . . . . . . . . . . . . . . . 54

    2.1 Torque and forces of electric dipoles in eletric fields . . 543 Atomic and molecular dipoles . . . . . . . . . . . . . . . . . . 55

    3.1 Induced dipole moments . . . . . . . . . . . . . . . . . 553.2 Permanent dipole moments . . . . . . . . . . . . . . . . 55

    4 Electric fields from polarized matter . . . . . . . . . . . . . . . 55

    11 Magnetic Phenoma in Matter 56

    12 Dielectrics and Refraction 57

    Bibliography 58

    5

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    Contents

    Abstract

    This is going to be a summary of Prof Simon Lillys lecture "PhysicsIII - Electricity and Magnetism" in order to look up the basic facts andformulas quickly. Its intention is not to replace the script from 2005[1] which is very close to Prof. Lillys notes and online available1.But of course this summary contains the basic deductions necessary tounterstand the material.

    In addition to the summarized lecture notes, I will add importantthings from the exercises (but give me some time to do this [and theexercises]).

    Note that this summary is very incomplete at the moment. I hopethat I can present something like a final version about 1-2 weeksafter the end of the semester.

    Please email2 me any errors in the sections which are not under con-struction.

    1http://mitschriften.amiv.ethz.ch/[email protected] oder [email protected]

    6

    http://mitschriften.amiv.ethz.ch/main.php?page=3mailto:[email protected]:[email protected]:[email protected]:[email protected]://mitschriften.amiv.ethz.ch/main.php?page=3
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    Chapter 1

    Basics

    1 Literature

    The lecture is based on the "Purcell" [5]. Prof. Lilly recommended also the"Jackson" [2] and the "Knzig" [3]. All references are listed in the bibliogra-phy at the end of this document.

    2 Constants and Units

    2.1 Constants

    electric permittivity 0 =1

    0c20

    = 8.854187 . . . 1012 AsVm

    (1.1)

    magnetic permeability 0 = 4107

    = 1.25663706144 . . . 106 Hm

    (1.2)

    elementary charge e = 1.60217733 . . . 1019C (1.3)mass of electron me = 9.1093826 1031kg (1.4)

    mass of proton mp = 1.67262171 1027kg (1.5)Boltzmanns constant k = 1.3806504(24) 1023 J

    K(1.6)

    = 8.617343(15) 105 eVK

    (1.7)

    7

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    1. Basics

    2.2 Units

    1 C = 1A s (Coulomb) (1.8)

    1 V = 1J

    C= 1

    W

    A= 1

    kg m2

    s3 A(Volt) (1.9)

    1 F = 1C

    V= 1

    A2 s4

    kg m2(Farad) (1.10)

    1 T = 1Vs

    m2= 1

    N

    Am= 1

    Wb

    m2= 1

    kg

    As2= 104Gs (Tesla) (1.11)

    1 H = 1Vs

    A = 1 s (Henry) (1.12)

    3 Terms

    We use some special terms and abbreviations, these things are declared here.

    EMF or emf is short for electro motive force. This is caused by mov-ing something through an electric or magnetic field, as defined in thecorresponding context.

    AC stands for Alternating Current and means that we apply a currentthat changes periodically with time, in our cases sinusoidally.

    DC stands for Direct Current and is used for currents which do notvary periodacally with time, in most cases a DC current is constant.DC currents can be damped, in this cases they are not constant any-more.

    4 Concept of charge

    two types of charge, named + and -

    different types attract, same types repel each other

    the total electric charge of an isolated system i

    qi is constant

    charge is relativistically invariant

    charge in nature is quantized in units of the elementary charge e

    8

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    Chapter 2

    Electrostatics

    1 Force

    1.1 Coulombs Law

    The force between two charges acts on the shortes connection (vector #r 12)between the two charges and is described by Coulombs Law:

    #

    F =q1 q2

    40r12#r 12 (2.1)

    Additivity

    The force on a charge x which located next to i other charges is the sum ofall forces.

    #

    Fx = i=x

    1

    40

    qxqir2xi

    #r xi (2.2)

    1.2 Energy of a charge

    If we bring a charge q1 next to another charge q2, we must do work on it.Therefore the charge has a stored energy

    W1 =

    r12

    #

    F 12 d#s = W2 (2.3)

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    2. Electrostatics

    Example: charges in NaCl

    To visualize the superposition priniciple, one can calculate the total enery ofan ion in a NaCl-crystal with lattice constant a :

    Wi =1

    2

    e2

    40

    6

    a+

    122a 8

    3a+

    6

    2a ...

    =

    1

    2

    1

    40

    1.748e2a

    (2.4)

    If we sum up all the N ions, we get

    W =1

    2

    1

    40

    1.748Ne2

    a

    (2.5)

    2 Eletric field

    The electric field is physical quantity, which is independent of the samplecharge.

    #

    E =

    #

    F

    q(2.6)

    #

    E =1

    40

    all space

    (x, y, z)r2

    #r dxdydz (2.7)

    2.1 Charge density

    The charge density is a helping quantity to get the (differential) charge per(differential) volume.

    =dF

    dq(2.8)

    (2.9)

    It can be expressed in terms of the potential and the electric field:

    = 0( #)2 (2.10) = 0

    #E (2.11)

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    2.2 Curl of the electric field

    Because the eletric field is conservative, the curl vanishes.

    rot#

    E = rot( #) = 0 (2.12)

    As a consequence from vector analysis, every closed path integral is 0.

    3 Flux

    The flux is defined as

    d := E d #a :=

    surface

    E d #a =E d #a (2.13)

    (2.14)

    The flux through a closed surface generated by charges outside of this sur-face is = 0.

    3.1 Flux and E-Fields of various charge distributions

    spherical uniformly charged symmetric sphere

    With the total charge qs and the surface charge density =qs

    4r2swe get

    inside: = 4r2E(r) =1

    0

    r0

    dV E = 0 (2.15)

    outside: = 4R2E(R) =qs0 E(R) = qs

    4R20(2.16)

    spherical uniformly charged cylinder

    tba

    11

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    2. Electrostatics

    infinite line charge

    With the total charge ql and the line charge denisity =qll we get

    = 2rl E(r) = l0 E(r) =

    2r0(2.17)

    infinite sheet charge

    Total and surface charge density like before, it follows:

    = 2r2 E(l) = r2

    0 E(l) =

    20(2.18)

    4 Gauss Law

    Gauss law relates the flux to the enclosed charge(s).

    4.1 integral form

    =S

    #

    E d #a =1

    0

    dV =

    i

    qi

    0(2.19)

    4.2 differential form

    div E =

    0(2.20)

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    5 Potential

    The electric potential is defined for every point of the room. It indicates theability to perform work.

    AB = B

    A

    #

    E d #s [] = 1V (Volt) (2.21)

    usual convention : () = 0 (see def. of pot.) (2.22)

    E = #

    (2.23)

    5.1 Definiton of potential 0

    Potential can be only expressed in difference to another point. To make iteasy, it is a usual convention to set the potential in equal to zero.

    () = limr (r) := 0 (2.24)

    5.2 Potential of radial-symmetrical charge distribution

    The potential for radial-symmetrical distributed charge (e.g. charged sphere)is

    =1

    40

    rd #r (2.25)

    5.3 Potential of multiple charges

    The potential of multiply charges is just the superposition of the seperatepotentials.

    (x, y, z) =1

    40

    N

    i=1

    qir

    =1

    40

    V

    (x, y, z)r

    d #x (2.26)

    13

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    2. Electrostatics

    5.4 Potential of a spherical shell

    The potential of a charged spherical shell with radius R and charge Q isgiven by

    (r) =1

    40

    Q

    r(r > R) (r) =

    1

    40

    Q

    R(r < R) (2.27)

    Inside the shell the potential doesnt change because there is no electric field.

    5.5 Potential of an electric dipole

    For an electric dipole made out of two charges |q1| = +q and |q2| = q at#x 1 = (0,0,

    l2 ) and

    #x 2 = (0,0, l2 ) the potential is given by

    (r, , ) =1

    40

    p cos()

    r2p = lq (2.28)

    p is called the dipole moment, is the angle between the z-axis and #r .With in spherical coordinates we obtain the following expressions for thecomponents of the electric field:

    Er = r

    E = 1r sin()

    E = 1r

    (2.29)

    6 Energy of an electric field

    W =02

    entire field

    E2 dV (2.30)

    enery density =0E2

    2(2.31)

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    Chapter 3

    Conductors

    1 Conductors and Insulators

    The mobility in conductors is about 1020 higher than in insulators. Be-cause of this mobility charges in the conductor can rearange and adopt toexternally applied eletric fields. Therefore the eletric field within vanishes:

    inside:#

    E = 0 (3.1)

    surface: = k = const.#

    E surface (3.2)

    2 General Electrostatic Problem

    The general electrostatic problem is, that we a system of conductors withsome charge on it and want to determine the electric field arround them.We can distinguish these 3 cases:

    1. k is defined ( Dirichlet problem)

    2. Qk is defined ( Neumann boundary conditions)

    3. a mix of the first two situations, which is not overdefined

    3 Uniqueness Theorem

    For a given situation, there is at most one solution.

    This holds in our contex for the general electrostatic problem, in which wewant to determine the eletric field arround one ore more conductors.

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    3. Conductors

    4 Potential and Field inside an empty cavity in a closed

    conductor

    Inside a cavity which is fully enclosed by a conductore we have no E-fieldinside and a constant potential on the surface:

    #

    E = const = const on the surface (3.3)

    solution: 2 = 0 = const in the cavity (3.4)

    5 Mirror principle

    We can use the uniqueness theorem to determine the influence of a chargebrought next to a conductor.

    [tba: nice image of the mirror principle and the electric field]

    Consider a charged in height h over an infinte sheet conductor:

    Ez,q+ =1

    40

    q(r2 + h2)

    cos Ez,q =1

    40

    q(r2 + h2)

    cos (3.5)

    cos = h(r2 + h2 Ez = 120 qh(r2 + h2)3/2 (3.6)

    It follows the surface charge distribution and the total charge on the sheet,which is q as expected:

    = 0Ez =1

    2

    qh(r2 + h2)3/2

    Qs =

    0

    2rd #r = q (3.7)

    Because of that, its called the mirror principle: Instead of thinking of theconductor and one charge, we think of two charges (see picture). The elet-

    ric field at the location of the conduction is the same and because of theuniqueness theorem we solved the problem.

    If the sheet is not infinite, the charges distribute like this: [tba: picture ofcharge distribution of not infinite sheet charge]

    6 conducting sphere in external field

    tba

    16

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    7 Capicatance and capacitors

    7.1 Definition of capicatance

    C =Q

    U(3.8)

    [C] = 1F = 1C

    V (3.9)

    7.2 Types of capacitors

    Plate capicator:

    E =F

    d E = 1 2

    d(3.10)

    = 0E (3.11) C = A0

    d(3.12)

    (3.13)

    Spherical capicator out of two spheres

    C =Q

    U=

    QQ

    40r1 Q

    40r2

    =40r1r2

    r1

    r2(3.14)

    Spherical capicator out of one sphere

    C = 40r1 (3.15)

    A single sphere as a capacitor is the limit of the spherical capicator with oneshell at r2 = .

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    3. Conductors

    Cylindrical capicator

    C =20l

    ln r1r2(3.16)

    7.3 Energy stored in a capicator

    E =1

    C

    Q0

    q dq =Q2

    2C

    U= QC=Q

    2=

    C2

    2(3.17)

    7.4 Systems of capicators

    If we have a system of conductors, its helpful to introduce a capicatance for

    each two conductors: Defining 1, 2, 3 defines#

    E throughout the system(by uniqueness), so Q1, Q2, Q3 are determined (and vice versa). We canimagine various states:

    State I: 2 = 3 = 0

    all charges are proportional to 1

    Q1 = C111 Q2 = C211 Q3 = C311 (3.18)

    State II: 1 = 3 = 0

    Q1 = C122 Q2 = C222 Q3 = C322 (3.19)

    State III: 1 = 2 = 0

    Q1 = C133 Q2 = C233 Q3 = C333 (3.20)

    By superposition, general solutions are a sum of these states I, II, III

    Q1 = C111 + C122 + C133 (3.21)

    Q2 = C211 + C222 + C233 (3.22)

    Q3 = C311 + C322 + C333 (3.23)

    (3.24)

    which we can write as

    Qi =3

    j=1

    Cijj i = 1, 2, 3 (3.25)

    where Cij is a matrix.

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    Chapter 4

    Currents

    1 Electric currents

    An electric current are (net-)charges in motion. In general, n charges of value

    q are passing through an area#

    A with an average speed #v , the current isdefined as

    1.1 Definition of the current

    I#A = nq#

    A #v (4.1)

    With the current density#

    J the current can be calculated by

    I =A

    #

    J d #a (4.2)

    Current density

    We define the current density

    #

    J = i niqi

    #

    v i [J] =G

    m2 (4.3)

    Closed surface

    If we have a closed surface, we get with Gausss law

    Is =A

    #

    J d #a =V

    div#

    J dv (4.4)

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    4. Currents

    If#

    J is time-independent, no charge moves:

    div#

    J = 0 #J = const (4.5)

    2 Ohms law and Resistance

    The motion of charges is proportional to the electric field:

    #

    J = #

    E (4.6)

    2.1 Resistance and conductivity

    is called the conductivity of the material.

    =

    #

    J#

    E[] =

    1

    m

    = 1A

    V

    m

    (4.7)

    The inverse of the conductivity is the resistivity.

    =1

    [] = 1m (4.8)

    Dont mix up resistivity with resistance, the resistivity is specific for eachplace. A resistance can be deteremined/measured between two points, it is

    depends on the resistivity of the material between the two points.

    2.2 Definiton of the resistance

    We define the resistance

    R =U

    I[R] = 1 = 1

    V

    A(4.9)

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    3 Resistance for various components

    3.1 Discrete component

    If we consider a discrete component of length l and with cross-section areaA, we get

    I =

    #

    J d #a = AJ U =

    #

    E d #s = El (4.10)

    R =

    El

    AJ

    =L

    A

    =L

    A

    (4.11)

    3.2 Spherical conductors

    For two spherical conductors with radius a and b with a material inbetweenwith constant resistivity we get [4]

    dR(r) = dr

    4r2 R =

    ba

    dr

    4r2=

    4(

    1

    a 1

    b) (4.12)

    3.3 Cylindrical conductiors

    For two cylindrical conductors with radius a and b and length (materialinbetween with constant resistivity as before) we get [4]

    dR(r) = dr

    2rl R =

    ba

    dr

    2rl=

    2lln(

    b

    a) (4.13)

    4 Resistances in circuits

    4.1 Parallel circuits

    [tba: image of parallel]

    Rres = i

    Ri (4.14)

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    4. Currents

    4.2 Series circuits

    [tba: image of series circuit]

    1

    Rres=

    i

    1

    Ri(4.15)

    4.3 Combined series and parallel circuits

    Any combination of parallel and series circuits is imaginable. We reduceany complicated circuit into a combination of series and parallel circuits. Itholds:

    1. Ohms law for each component

    For each component

    Ri =UiIi

    (4.16)

    2. Kirchhoffs law

    The sum of all currents arriving at one node vanishes:

    i

    Iin = 0 (4.17)

    3. Voltage through every loop

    The voltage through every closed loop in the circuit is 0:

    i

    Vloop = 0 (4.18)

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    5 Energy dissipation

    The energy dissipated when a charge Q moves through a potential V is

    E = VQ [E] = 1J = 1 Joule (4.19)

    P = V I =V2

    R= I2R [P] = 1W = 1 Watt (4.20)

    6 Sources of electromotive force: Voltaic cellEnergy can come from a chemical reaction in the voltaic cell, imagine achemical reaction as a voltage source.

    I =

    R + RiV = IRi (4.21)

    energy per unit charge emf= (4.22)(4.23)

    Some energy is released as heat, therefore Ri and V as the available energy.

    7 Circuits with capicators

    [tba: small image with one circuit containing one capacitor, one resistor andone switch]

    If we have a circuit with only one charged capacitor and one resistor, thecurrent flows and Q and V in the capacitor goes exponentially down.

    V =Q

    CI =

    I

    R= dQ

    dt(4.24)

    dQ

    dt =Q

    CR integrate: lnQ = t

    RC + C (4.25)

    Q = Q0e tRC I = dQdt

    =V0R

    etRC (4.26)

    (4.27)

    as an exercise one can show: (4.28)

    0

    V Idt =CV20

    2=

    Q202C

    =Q0V0

    2= energy stored at start (4.29)

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    Chapter 5

    Fields of moving charges

    1 General force on a moving charge

    #

    F = q#

    E + q #v #B (5.1)

    2 Charge invariance

    Charge is relativistically invariant.

    This is becuse of the number of charges doesnt change in a system acceler-ated to relativistic velocities, because we have the same charge at relativisticvelocities. Consider a 2 H+2 - and a

    4 He+-Ion. The have both 2 protons, 2neutrons and 1 electron but different masses. Although the mass differenceis measurable, there is no charge difference.

    3 Fields of moving charges

    4 Electric field for an accelarated charge

    For a charge moving with constand velocity, we have an E-field that is radialform where the particle is.

    If the particle accelerates or decelerates, the E-field for the particle is radialfrom where the particle would have been. Outside the sphere of radiusr = ct the field doesnt know that the charge has moved as the theorems ofspecial relativity state this.

    [drawing from page 26]

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    Energy in the spite

    UE =

    0E2

    2dV dv = 2R2 sin dR d (5.2)

    =0q

    2a2

    2(40)2c4c2[

    3

    4] UE =

    q2a2

    120c3(5.3)

    Force on moving charges

    Ex = Ex dpxdt = Exq = Exq (5.4)Ey = Ey

    dpxdt

    =Ey

    (5.5)

    result:

    E =qa sin

    40Rc2(5.6)

    5 Forces between moving charges - the magnetic force

    The force between a current in a conductor (i.e. many moving charges ofdensity lambda with a velocity vI result in a current I = v) and a stationarycharge moved perpendicular to the direction of the flowing current is

    F =1

    20

    Iqv

    rc2(5.7)

    This force is perpendicular to the movement of the charge and perpendicularto the direction of the flowing current.

    For the derivation, see [1]. This force is called magnetic force. Its orientationcan be determined by using the right-hand-rule and for currents in wires bythe kork-screw rule.

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    Chapter 6

    Magnetic fields

    1 Definition of magnetic field

    1.1 Lorentz force

    The magnetic field is defined by the force acting on a moving charge:

    #

    F = q#

    E + q( #v x#

    B ) (6.1)

    This is called the Lorentz force law, the first term is the electric field we knowalready from chapter 2, the second part is the magnetic field.

    This magnetic field comes from moving charges i.e. currents.

    1.2 Definition of B-field

    B =1

    40

    2I

    rc2= 0

    I

    2r[B] = 1T (6.2)

    with the magnetic permeability

    0 = 10c2== 1.25663706144 . . . 106 Hm (6.3)

    To determine the direction in space of the B-field, one can use the right-hand-rule and the right corkscrew rule.

    B I B E (6.4)

    [image of B field going into the paper]

    The magnetic field B comes from currents and acts on currents.

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    2 Force between two wires

    I1 = n1qv1 I2 = n2qv2 (6.5)

    B1 =0 I12d

    B2 =0 I22d

    (6.6)

    force per unit length = IB F1 = 0 I1 I2l2d

    = F2 (6.7)

    ni is number density of charges.

    3 Properties of the magnetic field

    For an infinite wire the B-field arround it is

    B =0 I

    2r(6.8)

    3.1 Amperes Law

    If we have a current I passing throught a loop, we have

    #

    B d #s = 0 I = 0

    S

    Jd #a (6.9)

    With Stokes theorem we can write

    S

    #

    F d#

    s = A

    rot F d#

    a rot#

    B = 0#

    J (6.10)

    Loops enclosing no currents

    In general it holds for any closed loop through which no current flows

    #

    B d #s = 0 (6.11)

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    6. Magnetic fields

    4 Magntic poles

    Because magnetic field lines do not end, it follows that there is no magneticmonopole (in contrast to that the eletric charge is a monopole).

    A

    #

    B d #a = 0 rot #B = 0 #J (6.12)

    5 Uniqueness theorem

    Given a#

    J(x, y, z), there is unique#

    B (x, y, z).

    div#

    B = 0 rot#

    B = 0#

    J (6.13)

    6 Vector potential

    6.1 Deduction

    We search for a potential for B. To get this, we start with a potential calledA:

    B = rot#

    A (6.14)

    It holds

    div#

    B = div(rot#

    A) = 0 (6.15)

    rot(rot#

    A) = 0#

    J (6.16)

    For each component one can deduce for each component

    2 Ax = 0 Jx Ax = 04

    space

    Jxr

    dV (6.17)

    The general formular follows with doing this for each component x, y, z.

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    6.2 General formula

    2 #A = 0 #J #A = 04

    space

    #

    J

    rdV (6.18)

    rot#

    A =#

    B (6.19)

    By the uniqueness theorem, we relate by this formula the-one-and-only Bwith A and therefore A is unique.

    6.3 Application to a current carrying wire

    d#

    A =I04r

    d#

    l =I04r

    #

    J dV d#

    B = rotd#

    A (6.20)

    d #B = rotd #A = I04

    rot(1

    rd

    #

    l ) (6.21)

    =

    I0

    4d#

    l

    1

    r=

    I0

    4d

    #

    l

    #

    r

    r2(6.22)

    This is called the Biot-Savart-Law.

    Biot-Savart-law

    For a conductor of the differential length dl carrying a current I we get adifferential B-field

    d#

    B = Id#

    l

    #

    r (0

    4r2) (6.23)

    The integral form of this law is

    #

    B (r) =04

    V

    #

    J(r)#r

    |r|3dV (6.24)

    The vector r points from the place where the current is to the place we wantthe expression for the B-field.

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    6. Magnetic fields

    6.4 General differentials

    Out of the last derivations, we get the following expressions for the generaldifferentials:

    d#

    B =#

    J #r 04r2

    dV (6.25)

    d#

    E = #

    r1

    4r20dV (6.26)

    7 Fields of rings and solenoids

    [image section 5.4, B-field straight up]

    We can apply the Biot-Savart-Law:

    on axis: Bz =0

    4(b2 + z2)

    Idl cos =

    04(b2 + z2)

    (2bI) cos (6.27)

    =0 Ib

    2

    2(b2 + z2)3/2(6.28)

    at z = 0: Bz =0 I

    2b(6.29)

    Solenoid with wire turns

    [picture of solenoid]

    We have n turns of wire per meter and therefore

    I = Inr d

    sin

    b

    r= sin (6.30)

    dBz =0

    2(

    r dnI

    sin )

    b2

    r3=

    0

    2In sin d (6.31)

    Bz = 02

    nI

    21

    sin d =02

    In(cos 1 cos 2) (6.32)

    long solenoid: 1 = 0 ; 2 = 2 Bz = 0nI (6.33)

    #

    B d #s = 0 I (6.34)

    calculated on axis; but Amperes Law also fine for all r within the solenoid

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    8 Change in B across a current sheet

    [picture of sheet charge]

    Remember that we have change in#

    E across a charge sheet (see...tba), so theE-fields are:

    #

    E 1 #E 2 = E = 0

    E = 0

    (6.35)

    pressure on sheet = ( E1 + E22 ) energy density = 12 0E2 (6.36)

    We define a surface current density

    #

    Jin #x direction [J] = 1A

    m(6.37)

    Now we consider the little loop l and Amperes law:

    #

    B d #s = (B1 B2)l = 0 #J l Bz = 0 JxB = 0 #J B = 0 (6.38)B = 0 (6.39)

    8.1 Energy density

    In general the energy density of the magnetic field is given by

    Energy density in B-field = 120

    B2 (6.40)

    Derivation

    We consider a sheet carrying a flowing current and want to determine thepressure on the sheet....[tba]

    [tba: picture form page 33]

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    6. Magnetic fields

    With the charge density n and the velocity v we get

    dF = B(y) (dybc)nq charge

    v (6.41)

    #

    B d#

    d s = b dB = 0 (b dynqv) current

    dB = 0nqv dy (6.42)

    dF = Bnqv dybc =bc

    0B dB (6.43)

    We get the total force:

    F =

    bc

    0

    B2

    B1

    B dB (6.44)

    Therefore the pressure is

    Pressure = P =F

    bc=

    1

    20(B22 B21) =

    1

    2(B1 + B2)(B1 B2) = 1

    2(B1 + B2)J

    (6.45)

    Considering p dV work if sheet moves to sheet.It follows that:

    Energy density in B-field =1

    20 B2

    (6.46)

    (Compare this to that of the E-field which is E =10

    2 E2).

    9 Hall effect

    [tba: Picture form page 34]

    If we consider a current flowing throught a conductor under the influenceof an E field. The moving charges are subject to the Lorentz force. In caseof a normal conductor (metals etc.) we have moving electrons moving toone side of the conductor until we have an equilibrium of the Lorentz forceon the moving charges and the electrostatic force of the already separatedcharges.

    q#

    E z + q(#v #B) = 0 (6.47)

    This phenomen can be used to determine what charges are moving in aconductor. Its called the Hall effect (1879)

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    10 How do E and B transform together?

    [tba: picture form page 34]

    10.1 Derivation

    In the lab fram:

    Ey = 0

    Bz = 0 j = v00 (6.48)

    v0 =v0 v1 v0v

    c2= c

    0 1 0

    =

    0restframe ofplates

    0 (6.49)

    0 is defined in the restframe and comes from v0 and 0 comes from the

    transformation to FWe have the transformation of:

    = 1 0 (6.50)

    With this we can write

    j = v0 = 1 0c0

    1 0 = v0 v (6.51)

    Ey = 0=

    0 0

    0= Ey Bz

    00c(6.52)

    = Ey cBz00c2

    = Ey vBz(6.53)

    Bz = 0 j = 0v0 0v = Bz c00Ey (6.54)

    = Bz (00)1/2Ey (6.55)= Bz

    cEy (6.56)

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    6. Magnetic fields

    10.2 General transformation

    In general (directions as in the picture) we get:

    Ex = Ex Ey = Ey cBz Ez = Ez + cBy (6.57)

    Bx = Bx By = By +

    cEz B

    z = Bz

    cEy (6.58)

    This was first derived 1905 by Einstein, it was a key step in joining the theoryof E and B fields.

    The general vectoriell relations are:

    E = E E = E + c B

    B = B B = B c1 E

    Note, that if there is a frame with B = 0, we get

    B = c1 E = c1 Ebut with B = B = 0 we even get

    B =

    c1E

    e.g a moving charge

    IfE = 0, then we getE = c B

    te be inserted/corrected:

    If there is any frame with

    #

    B = 0 (6.59)

    E = EE = E (6.60)

    B = 0 (6.61)#

    B = 1c #E #B perp =

    c

    #

    #E = c

    #

    E

    (6.62)

    If there is a force with#

    E = 0:

    #

    E = c #B (6.63)

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    Chapter 7

    Magnetic Induction

    1 Magnetic Induction

    The motion of conductors through magnetic fields can produces emf.

    [tba: picture from page 36]

    1.1 Isolated conductor

    We have an accumulation of charges at ends until

    #

    E int =#v

    #

    B Ey = vBz (7.1)

    In the rest-frame of the conductor we have:

    Ey = [Ey cBz] = vBz (7.2)Eint = Ey = vBz Eint = vBz (7.3)

    1.2 Loop of wire

    [tba: picture from page 36 below] If we consider a loop moved perpendicularto a B field, we have an inducted current in the loop. This comes from theforces f2 und f1 along the pieces of lenght l. We can consider a constantmagnetic field because one can prove that for an inhomegenous field we getthe same solution.

    E =

    BA

    q( #v #B) d #s = qvBl (7.4)

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    7. Magnetic Induction

    2 EMF - Electro motive force

    We define the electro motive force, short emf, as

    =work

    charge(7.5)

    In case of an isolated conductor (in our case our loop), we get the expression

    = vlB =

    d

    dt

    (7.6)

    With an inhomegenous field with B1 at one end and B2 at the second end ofthe conductor we get the same solution (proof in the lecture):

    = vl(B1 B2) (7.7)

    2.1 General emf (electro-motive force)

    In general, we have for the emf

    =

    ( #v #B ) d #s (7.8)

    cc

    3 Magnetic flux

    We define the magnetic flux through a loop as

    (t) :=S

    #

    B d #a (7.9)

    At later time we have

    (t + dt) =

    S+ds

    B d #s = (t) + d (7.10)

    The difference of the magnetic flux goes away (or in) as emf.

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    4 Faradays law of induction

    Faradays law of induction is known as

    Uind = ddt

    #

    B d#

    A ddt

    (7.11)

    It follows (see derivation)

    rot#

    E = #

    B

    t(7.12)

    A magnetic field with a change in time produces an electric whirl field.

    The magnetic field is not completely defined by this term as we can add

    some components with rot#

    E = 0.

    4.1 Derivation

    We start with a fixed loop in charging B (remember moving loop) and lookat it in the rest frame of the loop:

    [tba:picture from page 37]

    = v(B2 B1)l (7.13)[tba: second picture below]

    #

    E = #v #B because #E = 0 (Einstein transformation) (7.14)

    #

    E d#

    s = = lv(E1 E2) energy gain per unit charge as charge moves

    = v(B1 B2)l = = d

    dt

    (7.15)

    Static loop

    If we have a static loop, we can derive with Stokes theorem.C

    #

    E d #s = ddt

    S

    #

    B d #a rot #E = t

    #

    B (7.16)

    rot #E = Bt

    (7.17)

    This is conform with rot#

    E = 0 in electrostatics.

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    7. Magnetic Induction

    5 Lenz Law

    The emf drives I around the loop and Lenzs Law gives us the direction In

    the case B1 > B2,d

    dtis negative.

    In general we have

    The emf produces currents which act always to reduce the changein .

    Because of this we have to put in energy into our system to maintain aconstant current (E = I2R).

    This law was first stated by Heinrich Lenz in 1834. It is nothing more thana special case of the principle of Le Chatelier:

    "Any change in status quo prompts an opposing reaction in theresponding system."

    6 Mutual inductance

    [tba:picture] We consider the general case of two circuits at a small distance.A change in current in one circuit may produce a change in in the othercircuit and therefore produces emf.

    21 =S2

    #

    B 1 d#a2 = kI1 emf= 21 = d21

    dt= k dI1

    dt(7.18)

    We define the constant M = M21 as the mutual inductance, which has thefollowing units:

    [M] = 1Vs

    A= 1 s = 1 H = 1 Henry (7.19)

    One can proof with Stokes theorem, the mutual inductances of two loopsare equal (see [Skript] for that):

    M = M21 = M12 21 = 12 I1 = I2 (7.20)

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    7 Self inductance

    A change in the magnetic flux through a loop of wire causes a change in thecurrent flowing through the loop. We define the self-inductance via

    =d

    dt=: LI

    t(7.21)

    [L] = 1Vs

    A= 1s = 1H = 1 Henry (7.22)

    7.1 Circuits with self-inductance

    [tba: picture p.39]

    Charging the solenoid

    We close the switch at t = 0.

    0 L dIdt

    = RI 0 = RI+ L dIdt

    (7.23)

    The solution of this DGL is

    I =0R

    (1 e RL l (7.24)

    Decharging the solenoid without diode

    If we open the switch, the solenoid will release a very high emf. This veryhigh emf can produce high voltages (can be much higher than the usedvoltages).

    Decharging the solenoid with diode

    To prevent this, one can add a diode in the circuit:

    [tba: picture: circuit with diode]

    As a result, the magnetic field goes down exponentially. We can calculate

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    7. Magnetic Induction

    that by integration the DGL with boundary values I(t0) = I0 and t = t0.

    LdI

    dt+ RI = 0 I = I0e RL (tt0) (7.25)

    8 Energy in a magnetic field

    A magnetic field can store energy. In case of a solenoid we can store theenergy by buildung up the magnetic field with a voltage and obtain thestored energy by disconnecting the voltage source.

    We obtain the energy for a current loop or a solenoid in a circuit:

    Emagnetic =LI20

    2(7.26)

    I0 is current flowing through the loop/solenoid before we release the en-ergy (e.g. opening a switch).

    8.1 General term for any B-field

    Emagnetic =1

    0

    V

    B2 dV (7.27)

    8.2 Derivation of the energy stored in a solenoid

    We can derive this expression for the energy stored in magnetic field bysetting up a magnetic field inside a solenoid...

    [tba: Herleitung]

    9 Application: Magnetic field brake

    In an exercise (8.2 [4]), we had a moving rod in a magnetic field, the ends ofthe rod are connected to a resistance R. The emf produced by the magnetic

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    field decelerated the rod:

    = ddt

    = ddt

    S

    #

    B d#

    A = BL dxdt

    = BLv (7.28)

    I =

    R= BLv

    R F = BIL (7.29)

    eq. of motion: 0 =dv

    dt+

    (BL)2

    mRv v = v0e

    (BL)2mR t (7.30)

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    Chapter 8

    Alternating Currents

    1 Definitions for AC-circuits

    1.1 Quality factor

    Q =energy soted in system

    rate of energy loss = radians befoe energy goes down to 1

    e(8.1)

    For

    V = V0et cos(t)underdamped solution (8.2)

    The energy is V2

    et

    .

    dE

    dt= 2E (8.3)

    under-damped

    Q =

    2(8.4)

    for near to cirital LR since = R2L

    R2

    4L2 1 1RC .

    Q is related to a phase shift

    V = V0etcos(t) I = C dVdt

    (8.5)

    I = CV0et sin(t + ) 1cos

    = tan1

    =

    1

    Q(8.6)

    2 RCL circuit

    [tba: picture from page 43]

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    8. Alternating Currents

    With Kirchhoffs law:

    0 cos(t) = LdI

    dt+ RI(as before in DC case) (8.16)

    tan = LR

    = 1Q

    I0 =0

    (R2 + 2L2)(8.17)

    The current I lags behind with a phase shift and Ihas a reduced amplitudeI0. In case of a DC current these formulars still hold, the simply go over intothe DC-forumulas.

    [tba: graphic of I and 0]

    5 RC-circuit

    Similiar to the RL-circuit we get

    tan =1

    RCI0 =

    0

    (R2 + 1C

    2)

    (8.18)

    6 RLC-circuit

    VL = V1 V2 = L dIdt

    VC = QC

    (8.19)

    I = I0 cos(t + ) VL = I0L sin(t + )(8.20)

    VC = 1CIdt = I0

    Csin(t + ) (8.21)

    V = VL + VC = (L 1C

    )I= sin(t + ) (8.22)

    It is conform with

    LI0 sin(t + ) forL = L 12C

    (8.23)

    or1

    C= (L 1

    C) (8.24)

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    I0 =0

    R2 + L 1C2

    (8.25)

    for fixed 0 adn we get max I0 (and zero phase lag) when

    L =1

    C max = 1

    LC(8.26)

    [graph: resonance curve, see p.43]

    Power

    Power I2 Power halfes when (L 1C

    = R (8.27)

    Expanding at about max peak leeaks to the half-peak power consumptionof

    2

    max=

    R

    maxL=

    1

    Q(8.28)

    7 Application: Media player

    changable resistor change in I, therefore change in volume put in asolenoid bass boost capacitore boost in high frequencies[summary of all 3 cases with circuits]

    8 AC currents and voltages as complex numbers

    We can represent AC currents and voltages as complex numbers. For thisthe current has to vary sinusoidally with time and the components (L, C, R)have to respond linear to the voltage.

    ei = cos + i sin I = I0 cost + = Re(I0ei

    eit) (8.29)

    = complex number representating relative amp and phase relative to V

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    8. Alternating Currents

    It is easy to show that representation of sum of currents is equal to the sum

    of their representations. With this we can analyze arbitrarly complicatedcircuits.

    Usual rules (of circuits with R only):

    1. At any junction:

    Iin = 0 i

    I0,i cost + i = 0 (8.30)

    i

    I0ei = 0 (8.31)

    2. Arround any loop:

    Voltage chips = em f (8.32)

    for LR-circuit:

    V = 0 cost (8.33)

    I = I0 cost + (8.34)

    tan = LR

    (8.35)

    I0 =0

    R2 + 2E(8.36)

    We can write

    I = YV (all complex numbers) (8.37)

    with Y =ei

    R2 + 2E(admittance) Z =

    1

    Y(impedance) (8.38)

    Now:

    Y =1

    RZ = R for pure R (8.39)

    Y = iL Z = iL for pure L (8.40)Y = iC Z =

    iC

    for pure C (8.41)

    Laws for addition

    I = I1 + I2 Y = Y1 + Y2 for parallel circuit (8.42)V = V1 + V2 Z = Z1 + Z2 for series circuit (8.43)

    This is the same as adding resistors in R-circuits.

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    Example 1

    [graphics marker 7.1]

    I = YV = [YR + YC + YL]V (8.44)

    = 0[1

    R+ i(C 1

    L)] (8.45)

    Example 2

    [graphics marker 7.2]

    I =V

    Z=

    V

    ZR + ZL + ZC=

    V

    R + i(L 1C )(8.46)

    = arctan1

    R(

    1

    CL) (8.47)

    I0 =0

    R2 + (L 1C )2 (8.48)

    General for components in parallel

    [graphics marker 7.3]

    I0 = 0[1

    R+ i(C +

    1

    L] = arctan R(C 1

    L) (8.49)

    9 Power consumptation in AC current

    Instantaneous power consumptation = V I (8.50)

    Power on average =< V I> (8.51)

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    8. Alternating Currents

    For pure resistor circuit:

    < V I> =V20R

    < cos2 t >=V202R

    =I20 R

    2(8.52)

    V I = 0 I0 cost cos (t + ) (8.53)

    = 0 I0[cos2 t cos (cost sint

    cancels out

    sin )] (8.54)

    = 0 I0 < cos2 t > cos (8.55)

    10 Some other definition

    V = 0 cost :=

    20 cost (8.56)

    I = I0 cos (t + ) :=

    2I0 cos (t + ) (8.57)

    Power = 0 I0 12

    cos := 0 I0 cos (8.58)

    These second definitions are also possible but not used in the lecture. Theymay be found in some books.

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    9. Maxwells equations and electromagnetic waves

    C

    #

    B d #s = 0 I S

    rot#

    B d #s =S

    0#

    J d #s (9.8)

    I =dQ

    dt=

    d

    dt(A) = A0

    E

    t(9.9)

    rot B = 0 #J + 00 Et

    (9.10)

    Now: div(rot#

    B ) = div0#

    J + divE

    t00 = 0

    t+ 0

    t= 0 (9.11)

    0E

    t : = displacement current (9.12)

    2 Maxwells Equation

    div#

    E =

    0Coulombs Law Gauss Law (9.13)

    div#

    B = 0 no magnetic monopoles (9.14)

    rot#

    E = dB

    dt Faraday induciton (9.15)

    rot#

    B = 0#

    J + 00E

    tAmperes Law2 (9.16)

    div#

    J = t

    continuity equation for charge (9.17)

    (9.18)

    These equations are called Maxwells equations, stated by Maxwell in 1865which was before the Theory of Relativity, the nature of matter was under-stood and before the link between light and electromagnetism was discov-ered.

    3 Electromagnetic Waves

    There are wave-like solutions to Maxwells equations in vacuum.

    #

    E = #z E0 sin(ky t) #B = #x E0 sin(ky t) (9.19) rot #E = #x kE0 sin(ky t) rot #B = #z kE0 sin(ky t) (9.20)

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    In a complete empty space we get with Maxwells Euquations

    rot#

    E = #

    B

    trot

    #

    B =1

    c2#

    E

    t(9.21)

    Therefore Maxwells Euqations are forfilled with the following conditions:

    c =100

    =

    kE0 = cB0 (9.22)

    #

    E#

    B = 0 (9.23)

    0E20

    B200

    = 0 (9.24)

    #

    v #

    E #

    B (9.25)

    The directions of travel is#

    E #BMaxwell postulated that light is an electric and magnetic wave.

    4 Energy transport in electromagnetic waves

    dE = (

    0E2

    2 +

    1

    20 B2

    ) 1

    20E200=

    12 0E

    2

    dV (9.26)

    = 0E2 dV =

    1

    0B2 dV (9.27)

    This energy is equally split between the E-field and the B-field.

    average energy density = 0 < E2>=

    1

    0< B2 > (9.28)

    =1

    2

    0E20 =

    1

    0

    B20 (9.29)

    energy transport per unit average = 0 < E2> c =

    1

    0< B2 > (9.30)

    We introduce the Poynting Vector

    #

    S =c00

    #

    E #B (9.31)

    This vector gives back the instantaneous energy transport per unit area tothe transport direction.

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    9. Maxwells equations and electromagnetic waves

    5 Lorentz transformations of electromagnetic waves

    Ex = Ex Ey = Ey cBz Ez = Ez + cBy (9.32)

    Bx = Bx By = By + c

    1 Ez Bz = Bz c1 Ey (9.33)By simply calculating we can see

    E B = Ex Bx + Ey By + EzBz (9.34)= Ex Bx +

    2Ey cBzBy + c1Ez (9.35)

    + 2

    Ez + cByBz c1

    Ey (9.36)= Ex Bx +

    2(1 2)EyBy + EzBz (9.37)= E B (9.38)

    and

    E 2 c2B 2 = E2x + 2Ey cBz2 + 2E2z + cBy2 (9.39)

    c2B2x + 2By +

    cEz

    2

    + 2B2z

    cEy

    2

    (9.40)

    = E2 c2B2 (9.41)

    0E2 1

    0B2 = 0E2 1

    0B2 (9.42)

    If E and B are perpendicular in the frame F, then also in an other frameF. IfE2 = c2B2 in F, then also in F and an electromagnetic wave in F isan electromagnetic wave in F. In the frame of the wave let be Ey = E0,Bz = c1E0, then

    Ey = E0 c

    cE0 = E0(1 ) (9.43)

    Bz = E0c c E0 = E0c 1 (9.44)

    where

    (1 ) =

    1 1 +

    So as 1, E 0 and B 0. This means, the frame that moves withlight speed in direction of the wave, the wave simply doesnt exist anymore.Therefore, the Lorentz transformations actually does change the amplitudesof the fields (and of course not the wave speed).

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    Chapter 10

    Electric and Magnetic Fieldsin Mattter

    1 Dielectric Materials

    When a material is introduced into a capacitor, the capacitance changes.

    in vacuum: C =Q

    V(10.1)

    with material C = rC with > 1 (10.2)given V: Q = r Q (10.3)given Q: V = V

    r E = E

    r(10.4)

    r medium

    1 vacuum by definiton

    1.00-1.01 typical gases

    1.00059 air at 273 K and atmospheric presure

    20-80 typical liquids

    60 CH3OH

    80 water at 293 K

    2-10 typical solids

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    10. Electric and Magnetic Fields in Mattter

    2 electric dipoles

    For two displaced charges:

    #p = ql #r + (10.5)#p =

    #r dV (10.6)

    2.1 Torque and forces of electric dipoles in eletric fields

    Torque

    The torque on an electric dipole in an electric field is

    #

    N = #p #E (10.7)

    Work to align the dipole

    The work to align the dipole from the

    state to the

    state is

    W = pE (10.8)

    This is equal to the work necessary to align an arbitraly orientated dipole.

    Potential energy

    The potential energy of the dipole is given by

    potential energy = #p #E (10.9)

    Net force in external E-field

    The net force on the dipole in an external#

    E-field is

    #

    F =

    #pEx#pEy#pEz

    (10.10)

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    3 Atomic and molecular dipoles

    3.1 Induced dipole moments

    Atoms and molecules can act as dipoles under influence of an external elec-

    tric field. An eletric field#

    E causes a dipole moment

    #p = 40#

    E =9

    2a30 (10.11)

    The constant is called the atomic polarizability and a0 the Bohr radius (de-duction of the formular for in quantum mechanics lectures). This dipolemoment yields in an dielectric constant r 2

    Estimation of

    | #E int | e40a20

    z

    a Eext

    Eint Ee

    40a2(10.12)

    p = ez 40Ea30 (10.13)

    3.2 Permanent dipole moments

    Asymmetric molecules can have a not-vanishing #p also if there is no exter-

    nal#

    E because of the differently distributed charge in the molecule (partialcharges). As a result materials with polar molecules can have much biggerdieleletric constants, e.g. in case of H2O r 80.

    4 Electric fields from polarized matter

    Material emposed of aligned dipoles of average strength #p and a numberdensity N have a total dipole moment of

    #

    P tot =#p NdV =

    #

    P dV (10.14)

    with the density of polarization#

    P .

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    Chapter 11

    Magnetic Phenoma in Matter

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    Chapter 12

    Dielectrics and Refraction

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    Bibliography

    [1] Raphael Honegger. Physics III - Script of the lecture. VMP, 2005.

    [2] John David Jackson. Classical Electrodynamics. Wiley-VCH, 1998.

    [3] Werner Knzig. Elektrizitt und Magnetismus. vdf Hochschulverlag AG,2003.

    [4] Prof. Dr. Simon Lilly, editor. Physics III - Exercises, HS 2008.

    [5] Edward M. Purcell. Electricity and Magnetism (Berkeley Physics Course,Vol.2). McGraw Hill Higher Education, 1984.